Performance characteristics All specifications are in accordance with the data of jsc russian Aircraft Corporation



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MiG-35 (according to NATO codification: “Fulcrum-F” - “fulcrum”) is the Russian perspective multi-functional light fighter of the “4 ++” generation, the characteristics of which are as close as possible to the fifth generation.

The MiG-35 multifunctional complex is designed to gain air supremacy and deliver effective attacks with precision-guided weapons at ground and surface targets from outside the enemy’s air defense zone. Flight tests began in January 2017 and will pass until the end of 2018. In 2018, it was planned to begin state trials.
Performance characteristics

All specifications are in accordance with the data of JSC Russian Aircraft Corporation “Миг -35”
Specifications

Crew: 1 or 2 people

     Length: 17.32 m

Wing span: 12 m

Wing area: 42 m²

Height: 4.44 m

Weight:


       empty: 13,500 kg

       normal take-off weight: 18,500 kg

       maximum take-off weight: 29,700 kg [25]

       mass of domestic fuel: 5830 kg


Engine

Engine type: Turbofan dual-circuit with afterburner

Model: RD-33MK or its modification with UVT RD-33MKV with an all-angle deviation of the thrust vector (within + - 20 °).

Maximum traction: 2 × 9000 kgf


Flight characteristics
Maximum speed:

at altitude: 2560 km / h

by the ground: 1450 km / h [27]

Practical ceiling: 17500 m

Range with normal combat load: 1000 km

Range without refueling: with PTB 3500 km

Maximum operational overload: +10 G
Armament



Cannon: 30 mm GSh-30-1 aviation gun

Weapon suspension units: 9

Outboard weight: 6 t

Hanging weapons: all types of guided and uncontrolled ammunition "air-to-air" and "air-to-surface" weighing up to 500 kg.

MiG-35 (NATO kodiga ko'ra: "Fulcrum-F" - "fulcrum") - bu "4 ++" avlodining Rossiyaning istiqbolli ko'p funktsional yorug'lik qiruvchisi, ularning xususiyatlari beshinchi avlodga iloji boricha yaqinroq.

Ko'p funktsiyali MiG-35 majmuasi havo ustunligini ta'minlash va dushmanning havo mudofaasi zonasidan tashqarida, yerga va er yuzidagi nishonlarga aniq hujumlarni amalga oshirish uchun mo'ljallangan. Parvoz sinovlari 2017 yil yanvar oyida boshlangan va 2018 yil oxiriga qadar davom etadi. 2018 yilda davlat sinovlarini boshlash rejalashtirilgan edi.

Ishlash xususiyatlari

Barcha texnik xususiyatlar "Rossiya aviatsiya korporatsiyasi" OAJ ma'lumotlariga mos keladi


Texnik xususiyatlari

Ekipaj: 1 yoki 2 kishi

Uzunligi: 17,32 m

Qanot oralig'i: 12 m

Qanotning maydoni: 42 m²

Balandligi: 4.44 m

Vazni:

bo'sh: 13,500 kg



normal parvoz og'irligi: 18,500 kg

eng yuqori ko'tarish og'irligi: 29,700 kg [25]

mahalliy yoqilg'ining massasi: 5830 kg

Dvigatel


Dvigatel turi: Turbofan yonilg'i bilan ishlaydigan ikki pallali

Model: RD-33MK yoki uni UVT RD-33MKV yordamida tebranish vektorining har tomonlama burilishi (+ - 20 ° ichida).

Maksimal tortish: 2 × 9000 kgf

Uchish xususiyatlari

Maksimal tezlik:

balandlikda: 2560 km / soat

er tomonidan: soatiga 1450 km [27]

Amaliy ship: 17500 m

Oddiy jangovar yuklanish oralig'i: 1000 km

Yoqilg'i quyishsiz oralig'i: PTB bilan 3500 km

Maksimal operatsion yuk: +10 G

Qurol-yarog '



To'p: 30 mm GSh-30-1 aviatsiya tabancasi

Qurollarni to'xtatish moslamalari: 9

Tashqi og'irligi: 6 t

Osiladigan qurollar: og'irligi 500 kg gacha bo'lgan "havo-havo" va "havo-sirt" kabi barcha turdagi boshqariladigan va nazoratsiz o'q-dorilar.
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